karlos9796 karlos9796

25-05-2023
Physics

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Consider a turbojet engine mounted on a stationary test stand at sea level. The inlet and exit areas are t 1.0 atm, and 800 K respectively Calculate the static thrust of the engine
a.) Thrust-31880N
b.) Thrust 32680N
c.) Thrust -31600N
d.) Thrust- 3868 N

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